What was found
LT AFT FUSELAGE SKIN CHAFED AT STR 19L, BS 720D, 10". CUT-OUT DAMAGED AREA, FABRICATED DOUBLER AND STRUCTURAL FILLER, AND INSTALLED IAW SRM 53-30-1 FIG 5, 51-10-2, 51-30-8, AND 53-30-3 FIG 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT AFT FUSELAGE SKIN CHAFED AT STR 19L, BS 720D, 10". CUT-OUT DAMAGED AREA, FABRICATED DOUBLER AND STRUCTURAL FILLER, AND INSTALLED IAW SRM 53-30-1 FIG 5, 51-10-2, 51-30-8, AND 53-30-3 FIG 4.